高超声速飞机动力需求探讨

doi:10.7527/S1000-6893.2021.25798

Abstract

Abstract: With the great progress of hypersonic technology, especially under the background of the gradual engineering orientation of the scramjet technology, the discussion of hypersonic aircraft and its power system appears frequently in recent years. In order to operate in a wide flight speed range, combined power systems based on different thermal cycle modes have been proposed. As a result, there appear plenty of schools of systems in the development of hypersonic aircraft power, which poses a great challenge to the selection of hypersonic aircraft power system. Based on a review of aircraft development history and hypersonic related development technologies, this paper expounds the conclusion that combined power is the main development direction of hypersonic aircraft power at this stage. Aiming at the requirements of hypersonic aircraft, the working principle, working characteristics, advantages and disadvantages of several hypersonic combined power systems are sorted out and analyzed. Finally, the challenges to the future hypersonic aircraft research by using the combined power system are also predicted, as with the increase of flight speed, the integration of hypersonic aircraft and power is imperative.

Key words: hypersonic aircraft, combined power, Turbine-Based Combined Cycle (TBCC), Rocket-Based Combined Cycle (RBCC), ramjet, integration of aircraft and engine

CLC Number:

V236
V438

ZUO Linxuan, ZHANG Chenlin, WANG Xiao, LU Enwei, ZHU Wei. Requirement of hypersonic aircraft power[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(8): 525798-525798.

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[1]	Zeyong YIN, Yancheng YOU, Chengxiang ZHU, Jianfeng ZHU, Liaoni WU, Yue HUANG. Multi-ducted twin-turbines ejector-ramjet/scramjet combined cycle engine for hypersonic civil vehicles [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(2): 627181-627181.
[2]	LIN Peng, ZHUANG Fujian, QU Linfeng, XU Yangyang, SU Yadong. Technological development in hypersonic nozzle design, manufacture and validation: A review [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(6): 526160-526160.
[3]	LI Chaolong, XIA Zhixun, MA Likun, ZHAO Xiang, LUO Zhenbing, DUAN Yifan. Experiment on performance of solid rocket scramjet [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(12): 126075-126075.
[4]	MA Guangwei, SUN Mingbo, ZHAO Guoyan, LI Fan, LIANG Changhai, CHEN Huifeng. Simulation of scramjet with different wall temperatures and difference schemes [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(S1): 726353-726353.
[5]	LIU Zhikan, LIU Shenshen, LIU Xiao, ZENG Lei, DAI Guangyue. RBF data transfer based on physical gradient modification [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(7): 124506-124506.
[6]	CHEN Yile, YU Kaikai, XU Jinglei. New design method for scramjet nozzles with strong geometric constraints [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(6): 124259-124259.
[7]	ZHENG Zhonghua, FAN Zhouqin, WANG Ziang, YU Bin, ZHANG Bin. Numerical study of compressibility effect on flowfield evolution of vortex interaction [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(2): 123295-123295.
[8]	MENG Yu, GU Hongbin, SUN Wenming, ZHANG Xinyu. Microwave enhanced gliding arc plasma assisted supersonic combustion [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(2): 123345-123345.
[9]	CHEN Wenwu, HUANG Liya, XIA Zhixun, LI Pengfei. Theoretical performance and working parameters analysis of trans-medium ramjet [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(11): 123764-123764.
[10]	SUN Weiguo, SHI Ruihua, LIN Zuoming, LIU Daijun, ZHANG Wenshan, CAO Junwei, FAN Zhongguo, MA Conghui, FU Zechuan, LIU Aihua, TIAN Peng, QIAN Qinjian, CHEN Fei, DUAN Lei, CUI Jinping, LIANG Xiaojia. A ramjet based on solid-liquid phase change fuels [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(5): 122780-122780.
[11]	MENG Yu, GU Hongbin, ZHANG Xinyu. Influence of microwave on structure of supersonic combustion flame [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(12): 123224-123224.
[12]	GONG Lunkun, CHEN Xiong, LI Weixuan, YANG Haitao, ZHOU Changsheng. Influencing factors for self-sustained combustion of solid fuel ramjet [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2017, 38(7): 120821-120821.
[13]	LYU Duo, LU Haiying, ZHOU Jianjun, SHANG Shoutang, YU Xiao. Key technology for pre-cooler in near space vehicle propulsion system [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(S1): 119-126.
[14]	LI Xiang, FU Bo. Thermal test technique of complex structure of hypersonic aircraft [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(S1): 73-79.
[15]	WU Dafang, WANG Yuewu, SHANG Lan, PU Ying, WANG Huaitao. Test research and numerical simulation on thermal modal of plate structure in 1200℃ high-temperature environments [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(6): 1861-1875.